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1. 发明授权

US08979470B2 Gas turbine engine and method for cooling the compressor of a gas turbine engine 有权
标题翻译：燃气涡轮发动机和用于冷却燃气涡轮发动机的压缩机的方法
公开(公告)号：US08979470B2
公开(公告)日：2015-03-17
申请号：US13197840
申请日：2011-08-04
申请人： Sergei Riazantsev , Holger Kiewel , Sven Olmes , Thomas Kramer , Sergey Shchukin
发明人： Sergei Riazantsev , Holger Kiewel , Sven Olmes , Thomas Kramer , Sergey Shchukin
IPC分类号： F01D5/08 , F01D5/18 , F01D5/30 , F04D29/32 , F04D29/58
CPC分类号： F01D5/084 , F01D5/3007 , F04D29/321 , F04D29/584 , F05D2220/32
摘要： A gas turbine engine includes a compressor with rotor blades having roots connected into seats of a compressor drum. The rotor blade roots and/or the compressor drum have longitudinal passages for a cooling fluid, connecting higher pressure areas to lower pressure areas of the gas turbine engine.
摘要翻译：燃气涡轮发动机包括具有转子叶片的压缩机，转子叶片具有连接到压缩机鼓的座中的根部。转子叶片根部和/或压缩机滚筒具有用于冷却流体的纵向通道，将较高压力区域连接到燃气涡轮发动机的较低压力区域。

2. 发明申请

US20120036864A1 GAS TURBINE ENGINE AND METHOD FOR COOLING THE COMPRESSOR OF A GAS TURBINE ENGINE 有权
标题翻译：气体涡轮发动机和用于冷却气体涡轮发动机的压缩机的方法
公开(公告)号：US20120036864A1
公开(公告)日：2012-02-16
申请号：US13197840
申请日：2011-08-04
申请人： Sergei RIAZANTSEV , Holger Kiewel , Sven Olmes , Thomas Kramer , Sergey Shchukin
发明人： Sergei RIAZANTSEV , Holger Kiewel , Sven Olmes , Thomas Kramer , Sergey Shchukin
IPC分类号： F02C7/18 , F02C7/141
CPC分类号： F01D5/084 , F01D5/3007 , F04D29/321 , F04D29/584 , F05D2220/32
摘要： A gas turbine engine includes a compressor with rotor blades having roots connected into seats of a compressor drum. The rotor blade roots and/or the compressor drum have longitudinal passages for a cooling fluid, connecting higher pressure areas to lower pressure areas of the gas turbine engine.
摘要翻译：燃气涡轮发动机包括具有转子叶片的压缩机，转子叶片具有连接到压缩机鼓的座中的根部。转子叶片根部和/或压缩机滚筒具有用于冷却流体的纵向通道，将较高压力区域连接到燃气涡轮发动机的较低压力区域。

3. 发明授权

US07329086B2 Rotor shaft, in particular for a gas turbine 有权
标题翻译：转子轴，特别是用于燃气轮机
公开(公告)号：US07329086B2
公开(公告)日：2008-02-12
申请号：US11386497
申请日：2006-03-22
申请人： Markus Roland Wiebe , Thomas Kramer , Holger Kiewel
发明人： Markus Roland Wiebe , Thomas Kramer , Holger Kiewel
IPC分类号： F01D25/12
CPC分类号： F01D5/081 , F05D2250/14
摘要： A rotor shaft, particularly for a gas turbine, includes a cooling air supply disposed inside the rotor shaft and a plurality of cooling air ducts connected to the cooling air supply and extending essentially radially outward toward an outside of the shaft, wherein each of the cooling air ducts has an elliptic cross section.
摘要翻译：特别是用于燃气轮机的转子轴包括设置在转子轴内部的冷却空气供给装置，以及连接到冷却空气供应部并且基本径向向外朝向轴外侧延伸的多个冷却风道，其中每个冷却风管具有椭圆形截面。

4. 发明授权

US07628581B2 Rotating machine 有权
标题翻译：旋转机
公开(公告)号：US07628581B2
公开(公告)日：2009-12-08
申请号：US11276360
申请日：2006-02-27
申请人： Andrea De Simone , Jonas Fältström , Holger Kiewel , Thomas Kramer , Markus Roland Wiebe
发明人： Andrea De Simone , Jonas Fältström , Holger Kiewel , Thomas Kramer , Markus Roland Wiebe
IPC分类号： F04D29/08
CPC分类号： F01D5/30 , F01D5/303 , F01D5/3038 , F01D11/001 , F05D2240/60 , F05D2250/14
摘要： A rotating machine (10), in particular a compressor or turbine, has a rotor shaft (11) which is rotatable about an axis (20) and is provided with at least one slot (14). The mechanical stresses in the region of the slot are reduced in that the at least one slot (14) has a slot bottom (17) with an elliptic cross-sectional contour (24).
摘要翻译：旋转机器（10），特别是压缩机或涡轮机具有转子轴（11），该转子轴可绕轴线（20）旋转并且设置有至少一个槽（14）。槽的区域中的机械应力减小，因为至少一个槽（14）具有具有椭圆形横截面轮廓（24）的槽底（17）。

5. 发明申请

US20060197400A1 ROTATING MACHINE 有权
标题翻译：旋转机
公开(公告)号：US20060197400A1
公开(公告)日：2006-09-07
申请号：US11276360
申请日：2006-02-27
申请人： Andrea De Simone , Jonas Faltstrom , Holger Kiewel , Thomas Kramer , Markus Wiebe
发明人： Andrea De Simone , Jonas Faltstrom , Holger Kiewel , Thomas Kramer , Markus Wiebe
IPC分类号： H02K1/00
CPC分类号： F01D5/30 , F01D5/303 , F01D5/3038 , F01D11/001 , F05D2240/60 , F05D2250/14
摘要： A rotating machine (10), in particular a compressor or turbine, has a rotor shaft (11) which is rotatable about an axis (20) and is provided with at least one slot (14). The mechanical stresses in the region of the slot are reduced in that the at least one slot (14) has a slot bottom (17) with an elliptic cross-sectional contour (24).
摘要翻译：旋转机器（10），特别是压缩机或涡轮机具有转子轴（11），该转子轴可绕轴线（20）旋转并且设置有至少一个槽（14）。槽的区域中的机械应力减小，因为至少一个槽（14）具有具有椭圆形横截面轮廓（24）的槽底（17）。

6. 发明授权

US08517676B2 Welded rotor of a gas turbine engine compressor 有权
标题翻译：燃气涡轮发动机压缩机的焊接转子
公开(公告)号：US08517676B2
公开(公告)日：2013-08-27
申请号：US13463090
申请日：2012-05-03
申请人： Ernst Pauli , Thomas Kramer , Holger Kiewel
发明人： Ernst Pauli , Thomas Kramer , Holger Kiewel
IPC分类号： F04D29/044 , B21K25/00
CPC分类号： F01D5/063 , F01D5/082 , F05D2230/232 , Y10T29/4932 , Y10T29/49321 , Y10T29/49323
摘要： A rotor (1) of a gas turbine compressor comprises a multiplicity of welded-together rotor disks (3a, 3b, 4, 5), of which two or more rotor disks (3a, 3b), in a radially outer region (9′), are welded together, and, in a radially inner central region (9), are abutment-joined together. Via the abutment-joining of two rotor disks (3a, 3b), a heat flow (8) radially outward from the center of the rotor (1) is achieved so that the material temperature of the rotor (1) can be kept below a predetermined level during operation. As a result, the service life of the rotor (1) can be increased. In one embodiment, one rotor disk (3a), on its surface, additionally has a recess (7) which can be cooled from outside. The rotor disks (3a, 3b) according to the invention, which are welded and abutment-joined together, can especially be used at the last point in the flow direction of the compressor.
摘要翻译：燃气涡轮压缩机的转子（1）包括多个焊接在一起的转子盘（3a，3b，4,5），其中两个或更多个转子盘（3a，3b）在径向外部区域（9' ）焊接在一起，并且在径向内部中心区域（9）中被邻接连接在一起。通过两个转子盘（3a，3b）的邻接连接，实现了从转子（1）的中心径向向外的热流（8），使得转子（1）的材料温度可以保持在操作期间预定水平。结果，可以提高转子（1）的使用寿命。在一个实施例中，一个转子盘（3a）在其表面上另外具有可从外部冷却的凹部（7）。根据本发明的转子盘（3a，3b）可以在压缩机的流动方向的最后点特别地被焊接和邻接连接在一起。

7. 发明申请

US20070086884A1 Rotor shaft, in particular for a gas turbine 有权
标题翻译：转子轴，特别是用于燃气轮机
公开(公告)号：US20070086884A1
公开(公告)日：2007-04-19
申请号：US11386497
申请日：2006-03-22
申请人： Markus Wiebe , Thomas Kramer , Holger Kiewel
发明人： Markus Wiebe , Thomas Kramer , Holger Kiewel
IPC分类号： F03B11/00
CPC分类号： F01D5/081 , F05D2250/14
摘要： A rotor shaft, particularly for a gas turbine, includes a cooling air supply disposed inside the rotor shaft and a plurality of cooling air ducts connected to the cooling air supply and extending essentially radially outward toward an outside of the shaft, wherein each of the cooling air ducts has an elliptic cross section.
摘要翻译：特别是用于燃气轮机的转子轴包括设置在转子轴内部的冷却空气供给装置，以及连接到冷却空气供应部并且基本径向向外朝向轴外侧延伸的多个冷却风道，其中每个冷却风管具有椭圆形截面。

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